As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1022 BTW LONG 13RH-14 RH (FUS). SUMMARY OF NRC 00029: FUSELAGE SKIN STA Y=1022 WAS REPAIRED PER PRI 599215-14 REV. 2 AND ER/A 599215-14 REV ORIGINAL SECTION I: PERMANENET REPAIR. ACCOMPLISH REPETITIVE INSPECTION WITHIN EVERY 24 MONTH INTERVAL AFTER 19MAY22 PER ER/A 599215-14 REV ORIG. SEC II. (LP #2243616)